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EP2956566A1 - Method for depositing a corrosion-protection coating - Google Patents
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EP2956566A1 - Method for depositing a corrosion-protection coating - Google Patents

Method for depositing a corrosion-protection coating

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Publication number
EP2956566A1
EP2956566A1 EP14708611.0A EP14708611A EP2956566A1 EP 2956566 A1 EP2956566 A1 EP 2956566A1 EP 14708611 A EP14708611 A EP 14708611A EP 2956566 A1 EP2956566 A1 EP 2956566A1
Authority
EP
European Patent Office
Prior art keywords
substrate
cement
coating
cementum
cavities
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP14708611.0A
Other languages
German (de)
French (fr)
Other versions
EP2956566B1 (en
Inventor
Nicolas Richet
Thierry Mazet
Michel VILASI
Stéphane MATHIEU
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Centre National de la Recherche Scientifique CNRS
Institut National Polytechnique de Lorraine
LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
Original Assignee
Centre National de la Recherche Scientifique CNRS
Institut National Polytechnique de Lorraine
LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Centre National de la Recherche Scientifique CNRS, Institut National Polytechnique de Lorraine, LAir Liquide SA pour lEtude et lExploitation des Procedes Georges Claude filed Critical Centre National de la Recherche Scientifique CNRS
Publication of EP2956566A1 publication Critical patent/EP2956566A1/en
Application granted granted Critical
Publication of EP2956566B1 publication Critical patent/EP2956566B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/36Embedding in a powder mixture, i.e. pack cementation only one element being diffused
    • C23C10/48Aluminising
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/04Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/52Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in one step
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/28Solid state diffusion of only metal elements or silicon into metallic material surfaces using solids, e.g. powders, pastes
    • C23C10/34Embedding in a powder mixture, i.e. pack cementation
    • C23C10/52Embedding in a powder mixture, i.e. pack cementation more than one element being diffused in one step
    • C23C10/54Diffusion of at least chromium
    • C23C10/56Diffusion of at least chromium and at least aluminium
    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C10/00Solid state diffusion of only metal elements or silicon into metallic material surfaces
    • C23C10/60After-treatment

Definitions

  • the present invention relates to the production of a protective coating against corrosion on a substrate having cavities.
  • Thermal spraying techniques such as plasma or flame projection involves sending molten or partially melted particles, at high speed, to the surface of the part to be protected.
  • the coating is constructed in successive layers. These techniques can only be used on open or easily accessible surfaces.
  • the vapor phase deposition techniques use a gaseous precursor of the coating to be produced.
  • This precursor may be produced in the direct vicinity of the surface to be coated (carburized pack) or transported via a gas to the surface to be coated (out of pack, CVD from a bottle or gaseous mixture, etc.).
  • the main difficulties encountered for the carburizing pack are related to the filling of parts having a complex geometry or very small dimensions (a few mm) with the cementum powder (precursor mixture of the coating).
  • the main limitations of the techniques using gaseous precursors concern the rapid depletion of the gaseous mixture in reactive species resulting in heterogeneities of chemical composition and / or thickness of the coating. It is very difficult to obtain a homogeneous coating on large surfaces or in complex geometries.
  • Physical vapor deposition techniques involve evaporating the component (s) of the coating prior to condensing them on the surface of the part to be coated. Evaporation is usually done by bombarding a target with a high energy beam (electrons or ions). The distance between the target and the surface to be coated is a major parameter for the homogeneity of the thickness of the deposit. These techniques are very difficult to use on parts of complex geometry or on non-accessible surfaces.
  • the carburizing pack is a very old process for making a coating on a part.
  • the latter is placed in a bed of cementum powder, which is a mixture of products capable of generating a reactive atmosphere at high temperature.
  • This cementum should be placed close to the surface to be coated to produce a homogeneous coating in thickness and chemical composition.
  • Coatings are conventionally made on parts having cavities of a few centimeters by filling the part with the cementum powder.
  • a problem is to improve the deposition processes by pack cementation to allow their use for the substrate coating having cavities.
  • a solution of the present invention consists in the use of a cementum in a pack-cementation deposition process on a substrate having cavities of minimum equivalent diameter e cm , characterized in that the cementum consists of spherical particles presenting each a diameter d such that d ⁇ e cm / 10.
  • the size of the cement particles can be measured by laser granulometry or sieves to ensure that no particle or agglomerate of cement particles exceeds the maximum size required.
  • a disagglomeration step may be necessary to "break" the agglomerates of elementary particles that may exceed the maximum size required.
  • the equivalent diameters of the particles are conventionally comprised between ⁇ at 1 mm, preferably between ⁇ at ⁇ .
  • the equivalent diameter is defined as the diameter of the cylinder or circle that fits into the smallest section giving access to the surface to be coated. Indeed, the latter does not necessarily have a standard form. Depending on the case, the use according to the invention may have one or more of the following characteristics:
  • the cementum consists of spherical particles each having a diameter d such that d ⁇ e cm / 10.
  • the cementum comprises a precursor of the element to be deposited, an activating agent and an inert diluent
  • the cementum comprises 10 to 60% of metal powder as precursor of the element to be deposited, 5 to 40% of activating agent, and a complement of 100% of inert diluent, the inert diluent preferably comprising refractory oxides,
  • the metal powder is made of aluminum or a mixture of aluminum with particles of Ni x Al y or of
  • the cementum comprises a precursor of the element to be deposited, a stripping flux, and an inert diluent.
  • the cement comprises an organic or inorganic binder.
  • the organic binder may be PVA polyvinyl acetate and the inorganic binder may be SiO 2.
  • the organic or inorganic binder be used during a step of atomizing the powder mixture. This optional step improves the flowability of the powder and thus the filling of the piece. It is to form spherical agglomerates of the powder mixture. This step will preferably be carried out under an inert atmosphere in order to prevent the surface oxidation of the metal powders which may be harmful for the deposition.
  • the inert compound does not chemically intervene in the formation of the coating. Its main function is to avoid the densification of the cementum which would prevent its elimination after deposit. It is usually a very stable refractory compound. Its content is the complement of the other two.
  • the solution according to the invention allows the realization of a deposit by pack cementation on parts of complex geometry and in inaccessible cavities.
  • the cementum used in the context of the invention has a very good flowability to fill the smallest gaps (diameter ⁇ 1mm) and distribute evenly within the entire cavity to be coated.
  • the particle size distribution and the morphology of the cement particles are the main parameters to ensure a good flowability of the mixture.
  • the particle size distribution is adjusted according to the equivalent diameter of the smallest passage of the cavity.
  • morphology spherical shapes which can be obtained by different grinding techniques for powders or powder mixture.
  • An atomization treatment of the powder mixture may also be used to form spheres of the powder mixture.
  • organic additives may be used to ensure a good cohesion of the spheres and a homogeneous dispersion of the elements of the mixture.
  • the present invention also relates to two methods of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm .
  • the first method of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm comprises the following successive steps:
  • step b) introducing into the cavities of the substrate the cementum prepared in step a) by a vibratory system;
  • the substrate-cement element is heated to a temperature below the melting temperature of the metal powder for a period of at least 6 hours at about 650 ° C for aluminum.
  • the substrate-cement element is heated to a temperature of between 900 ° C. and 1150 ° C., preferably greater than 980 ° C.
  • step c) the substrate-cement element is heated at about 650 ° C. for at least 6 hours.
  • the first method may have one or more of the following characteristics:
  • the particles of the cementum prepared in step a) are pre-activated by mechano-synthesis; preactivation makes it possible to increase the chemical reactivity of the precursor particles.
  • This treatment facilitates the reaction between the precursor and the activator and therefore the deposition.
  • the coating recovered in step g) comprises NiAl
  • the coating recovered in step g) has a thickness of between 15 and
  • the second method of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm comprises the following successive steps:
  • a cementitious consisting of a stripping flux and spherical particles of an inert diluent and a metal powder is prepared, said spherical particles each having a diameter d such that d ⁇ e cm / 10;
  • step b) introducing into the cavities of the substrate the cementum prepared in step a) by a vibratory system;
  • the substrate-cementation unit is heated to a temperature above the melting temperature of the pickling stream, under a primary vacuum or under an inert atmosphere (Ar), for a period of between 10 min and 2 h;
  • the cement is subjected to a washing step so as to remove the cement residue
  • the second method may have one or more of the following characteristics:
  • the washing step e) is carried out by means of an acidified aqueous solution.
  • the coating recovered in step f) comprises NiAl 3 .
  • said process comprises, before step e), a step of heating the substrate-cementation unit at a temperature of between 900 ° C. and 1150 ° C., preferably greater than 980 ° C.
  • the coating recovered in step f) comprises NiAl.
  • the coating recovered in step f) has a thickness between 5 ⁇ and 200 ⁇ , preferably between 5 ⁇ and 80 ⁇ .
  • FIG 1 shows schematically the different steps of the first method according to the invention.
  • the first process consists in the use of a powder mixture consisting of the activating agent (5%), an inert diluent (Alumina, silica, etc.) and a metal to be deposited, a metal powder ( between 10 and 60%) which may be either pure aluminum or an Al + NIA1 or AlCr mixture and whose particles may or may not have been "pre-activated” by mechano-synthesis.
  • the granulometry of the mixture is then adjusted so that it can be introduced into the channels by a vibratory system.
  • the assembly is then brought to a temperature below the melting temperature of the metal to be deposited for a period of at least 6 hours.
  • the assembly is again subjected to a vibration step for extracting the residual powder.
  • the coating consists of a surface enrichment of aluminum substrate whose composition is close to NiAl 3 .
  • the thicknesses obtained vary between 5 and 10 ⁇ depending on the time during which the first heating step was carried out.
  • the part thus coated is brought to a temperature of between 900 ° C. and 1150 ° C., preferably greater than 980 ° C., so as to obtain the NiAl composition in a superficial edge of thickness ranging from 15 to 25 ⁇ m ( Figure 3).
  • FIG. 2 schematizes the different steps of the second method according to the invention.
  • the second method consists in the use of a powder mixture consisting of a low-melting pickling flux (K A1F 6 -KA1F 4 ) which is the element which has the lowest melting point of the mixture constituting the cement and particles of an inert diluent and a pure metal powder or aluminum alloy. (10 to 60% of metal powders, 40% of stripping flux and the balance of inert diluent).
  • K A1F 6 -KA1F 4 low-melting pickling flux
  • the whole is introduced by vibration as in the case of the first method and is heated to a high temperature, lower than the melting of the metal phase, but greater than that of the stripping flux for a time that varies from a few minutes to one or two hours. .
  • the coating is obtained either under primary vacuum or inert controlled atmosphere (argon).
  • the residues are then extracted by washing directly after the heat treatment step.
  • the apparatus can be washed with a chemical solution (acidified aqueous).
  • the coating thus obtained corresponds to a phase of composition close to NiAl which can be converted into NiAl in a subsequent annealing step at a temperature between 900 ° C and 1150 ° C, preferably at 980 ° C.
  • the appearance of the coating is shown in FIG.
  • the powder mixtures can be stored for long periods of time in a desiccator under a primary vacuum or in a dry chamber under a neutral gas sweep and are immediately ready for use.
  • the inert diluent is selected from powders of refractory inert materials, more preferably from refractory mineral oxides, such as alumina, silica, magnesia and mixtures thereof, which are commonly used in cementation.
  • refractory inert materials more preferably from refractory mineral oxides, such as alumina, silica, magnesia and mixtures thereof, which are commonly used in cementation.
  • the substrate which can be provided with such a coating is generally chosen from metal substrates, for example iron or nickel base, alloy (s) substrates or superalloy (s), composite substrates comprising one or more metals and / or alloy (s) and / or superalloy (s) containing Ni to react with the deposited Al and form NiAl.
  • metal substrates for example iron or nickel base, alloy (s) substrates or superalloy (s), composite substrates comprising one or more metals and / or alloy (s) and / or superalloy (s) containing Ni to react with the deposited Al and form NiAl.
  • the substrate may be previously superficially enriched in Ni for example by electrolytic deposition.
  • the treatments are generally carried out under a neutral or reducing atmosphere, for example under an atmosphere of hydrogen and / or argon, preferably under an argon atmosphere, or under an argon atmosphere with, for example, from 5 to 10% of argon. hydrogen.
  • the pressure used during the treatment may be atmospheric pressure or a reduced pressure, for example a pressure of 10 " atm of argon.
  • the coatings obtained by the processes according to the invention give the substrates an excellent resistance to corrosion, even within each substrate cavity regardless of its size.
  • the photos of FIG. 3 show two samples of HR120 alloy, one (the one on the right) coated with the coating produced according to the second method according to the invention and the other (the left one) uncoated. These samples were subjected to a corrosive atmosphere consisting of (in% vol.): 15% CO, 5% CO 2 , 55% H 2 , 25% H 2 O, at a pressure of 21 bar absolute and a temperature of 650 ° C. After 4700 hours of exposure, it is clear that the coating deposited according to the second method of the invention can protect the alloy from corrosion.

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  • Chemical & Material Sciences (AREA)
  • Mechanical Engineering (AREA)
  • Organic Chemistry (AREA)
  • Metallurgy (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Thermal Sciences (AREA)
  • Physics & Mathematics (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
  • Powder Metallurgy (AREA)
  • Chemically Coating (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

The invention relates to the use of a cement in a method for pack-cementation deposition on a substrate containing cavities having a minimum equivalent diameter ecm, characterised in that the cement is formed by spherical particles each having a diameter d such that d ≤ ecm/10.

Description

Procédé de dépôt d'un revêtement contre la corrosion  Method of depositing a coating against corrosion

La présente invention est relative à la réalisation d'un revêtement protecteur contre la corrosion sur un substrat présentant des cavités. The present invention relates to the production of a protective coating against corrosion on a substrate having cavities.

Les techniques de réalisation de revêtements peuvent se classer en trois grandes familles :  The techniques of realization of coatings can be classified in three great families:

- la projection thermique,  - the thermal projection,

- le dépôt chimique en phase vapeur, et  chemical vapor deposition, and

- le dépôt physique en phase vapeur.  - the physical vapor deposition.

Les techniques de projection thermique comme la projection plasma ou flamme consiste à envoyer des particules fondues ou partiellement fondues, à grande vitesse, à la surface de la pièce à protéger. Le revêtement est construit par couches successives. Ces techniques ne sont utilisables que sur des surfaces ouvertes ou facilement accessibles.  Thermal spraying techniques such as plasma or flame projection involves sending molten or partially melted particles, at high speed, to the surface of the part to be protected. The coating is constructed in successive layers. These techniques can only be used on open or easily accessible surfaces.

Les techniques de dépôt en phase vapeur utilisent un précurseur gazeux du revêtement à réaliser. Ce précurseur peut être produit à proximité directe de la surface à revêtir (pack cémentation) ou être transporter via un gaz sur la surface à revêtir (out of pack, CVD à partir de bouteille ou mélange gazeux,...). Les principales difficultés rencontrées pour le pack cémentation sont liées au remplissage de pièces présentant une géométrie complexe ou de très petites dimensions (quelques mm) avec la poudre de cément (mélange précurseur du revêtement). Les principales limitations des techniques utilisant des précurseurs gazeux concernent l'appauvrissement rapide du mélange gazeux en espèces réactives entraînant des hétérogénéités de composition chimique et/ou d'épaisseur du revêtement. Il est très difficile d'obtenir un revêtement homogène sur de grandes surfaces ou dans des géométries complexes.  The vapor phase deposition techniques use a gaseous precursor of the coating to be produced. This precursor may be produced in the direct vicinity of the surface to be coated (carburized pack) or transported via a gas to the surface to be coated (out of pack, CVD from a bottle or gaseous mixture, etc.). The main difficulties encountered for the carburizing pack are related to the filling of parts having a complex geometry or very small dimensions (a few mm) with the cementum powder (precursor mixture of the coating). The main limitations of the techniques using gaseous precursors concern the rapid depletion of the gaseous mixture in reactive species resulting in heterogeneities of chemical composition and / or thickness of the coating. It is very difficult to obtain a homogeneous coating on large surfaces or in complex geometries.

Les techniques de dépôt physique en phase vapeur consistent à faire évaporer le ou les éléments constitutifs du revêtement avant de les condenser à la surface de la pièce à revêtir. L'évaporation se fait en général en bombardant une cible avec un faisceau de forte énergie (électrons ou ions). La distance entre la cible et la surface à revêtir est un paramètre majeur pour l'homogénéité de l'épaisseur du dépôt. Ces techniques sont très difficilement utilisables sur des pièces de géométrie complexe ou sur des surfaces non accessibles.  Physical vapor deposition techniques involve evaporating the component (s) of the coating prior to condensing them on the surface of the part to be coated. Evaporation is usually done by bombarding a target with a high energy beam (electrons or ions). The distance between the target and the surface to be coated is a major parameter for the homogeneity of the thickness of the deposit. These techniques are very difficult to use on parts of complex geometry or on non-accessible surfaces.

L'intensification des procédés industriels conduit à utiliser les matériaux dans des conditions de plus en plus sévères et à réduire la taille des pièces mises en œuvre. Dans la plupart des cas, il est nécessaire de protéger les pièces de leur environnement avec un revêtement. Comme présenté dans les paragraphes précédents, les géométries complexes et les surfaces non accessibles posent des problèmes pour la réalisation de revêtements avec les techniques traditionnelles. The intensification of industrial processes leads to the use of materials under increasingly stringent conditions and to reduce the size of the parts used. In most cases, it is necessary to protect the parts of their environment with a coating. As presented in the previous paragraphs, the complex geometries and non accessible surfaces pose problems for the realization of coatings with the traditional techniques.

Il est donc nécessaire de développer de nouvelles techniques de dépôt ou d'adapter les techniques existantes aux nouvelles contraintes.  It is therefore necessary to develop new deposit techniques or adapt existing techniques to the new constraints.

Le pack cémentation est un procédé très ancien pour réaliser un revêtement sur une pièce. Cette dernière est placée dans un lit de poudre de cément, qui est un mélange de produits capables de générer une atmosphère réactive à haute température. Ce cément doit être placé à proximité de la surface à revêtir pour produire un revêtement homogène en épaisseur et en composition chimique. Des revêtements sont classiquement réalisés sur des pièces présentant des cavités de quelques centimètres en remplissant la pièce avec la poudre de cément.  The carburizing pack is a very old process for making a coating on a part. The latter is placed in a bed of cementum powder, which is a mixture of products capable of generating a reactive atmosphere at high temperature. This cementum should be placed close to the surface to be coated to produce a homogeneous coating in thickness and chemical composition. Coatings are conventionally made on parts having cavities of a few centimeters by filling the part with the cementum powder.

Cependant lorsque les cavités ont des tailles caractéristiques de l'ordre du millimètre, et des rapports d'aspect (ratio longueur / largeur) élevés, l'introduction du cément est beaucoup plus complexe. C'est pourquoi, les procédés à partir de poudre, de type pack cémentation sont généralement utilisés pour des pièces ne présentant pas ou peu de zone difficile d'accès.  However, when the cavities have characteristic sizes of the order of a millimeter, and aspect ratios (ratio length / width) high, the introduction of the cement is much more complex. This is why processes using powder, type pack cementation are generally used for parts with no or little hard to access area.

Dès lors, un problème qui se pose est d'améliorer les procédés de dépôt par pack- cémentation afin de permettre leur utilisation pour le revêtement de substrat présentant des cavités.  Therefore, a problem is to improve the deposition processes by pack cementation to allow their use for the substrate coating having cavities.

Une solution de la présente invention consiste en l'utilisation d'un cément dans un procédé de dépôt par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm, caractérisé en ce que le cément est constitué de particules sphériques présentant chacune un diamètre d tel que d < ecm/10. A solution of the present invention consists in the use of a cementum in a pack-cementation deposition process on a substrate having cavities of minimum equivalent diameter e cm , characterized in that the cementum consists of spherical particles presenting each a diameter d such that d <e cm / 10.

La taille des particules de cément peut être mesurée par granulométrie laser ou à l'aide de tamis afin de s'assurer qu'aucune particule ou agglomérat de particules de cément ne dépasse la taille maximale requise.  The size of the cement particles can be measured by laser granulometry or sieves to ensure that no particle or agglomerate of cement particles exceeds the maximum size required.

Une étape de désagglomération peut être nécessaire afin de « casser » les agglomérats de particules élémentaires qui peuvent dépasser la taille maximale requise.  A disagglomeration step may be necessary to "break" the agglomerates of elementary particles that may exceed the maximum size required.

Les diamètres équivalents des particules sont classiquement compris entre Ιμιη à 1mm, préférentiellement entre Ιμιη à ΙΟΟμιη.  The equivalent diameters of the particles are conventionally comprised between Ιμιη at 1 mm, preferably between Ιμιη at ΙΟΟμιη.

Le diamètre équivalent est défini comme le diamètre du cylindre ou du cercle qui s'inscrit dans la section la plus petite donnant accès à la surface à revêtir. En effet, cette dernière n'a pas nécessairement une forme standard. Selon le cas, l'utilisation selon l'invention peut présenter une ou plusieurs des caractéristiques suivantes : The equivalent diameter is defined as the diameter of the cylinder or circle that fits into the smallest section giving access to the surface to be coated. Indeed, the latter does not necessarily have a standard form. Depending on the case, the use according to the invention may have one or more of the following characteristics:

- le cément est constitué de particules sphériques présentant chacune un diamètre d tel que d < ecm/ 10. the cementum consists of spherical particles each having a diameter d such that d <e cm / 10.

- le cément comprend un précurseur de l'élément à déposer, un agent activant et un diluant inerte  the cementum comprises a precursor of the element to be deposited, an activating agent and an inert diluent

- le cément comprend 10 à 60% de poudre métallique comme précurseur de l'élément à déposer, 5 à 40% d'agent activant, et un complément à 100% de diluant inerte, le diluant inerte comprenant de préférence des oxydes réfractaires,  the cementum comprises 10 to 60% of metal powder as precursor of the element to be deposited, 5 to 40% of activating agent, and a complement of 100% of inert diluent, the inert diluent preferably comprising refractory oxides,

- la poudre métallique est constituée d'aluminium ou d'un mélange d'aluminium avec des particules de NixAly ou de the metal powder is made of aluminum or a mixture of aluminum with particles of Ni x Al y or of

- le cément comprend un précurseur de l'élément à déposer, un flux de décapage, et un diluant inerte.  the cementum comprises a precursor of the element to be deposited, a stripping flux, and an inert diluent.

- le cément comprend un liant organique ou inorganique. Le liant organique peut être du PVA Poly acétate de vinyle et le liant inorganique peut-être du Si02. En effet, le liant organique ou inorganique être utilisé lors d'une étape d'atomisation du mélange de poudre. Cette étape facultative permet d'améliorer la coulabilité de la poudre et donc le remplissage de la pièce. Il s'agit de former des agglomérats sphériques du mélange de poudre. Cette étape sera réalisée de préférence sous atmosphère inerte pour éviter l'oxydation de surface des poudres métalliques qui peut être néfaste pour le dépôt.  the cement comprises an organic or inorganic binder. The organic binder may be PVA polyvinyl acetate and the inorganic binder may be SiO 2. Indeed, the organic or inorganic binder be used during a step of atomizing the powder mixture. This optional step improves the flowability of the powder and thus the filling of the piece. It is to form spherical agglomerates of the powder mixture. This step will preferably be carried out under an inert atmosphere in order to prevent the surface oxidation of the metal powders which may be harmful for the deposition.

Le composé inerte n'intervient pas chimiquement dans la formation du revêtement. Sa fonction principale est d'éviter la densification du cément qui empêcherait son élimination après dépôt. C'est en général un composé réfractaire très stable. Sa teneur est le complément des deux autres.  The inert compound does not chemically intervene in the formation of the coating. Its main function is to avoid the densification of the cementum which would prevent its elimination after deposit. It is usually a very stable refractory compound. Its content is the complement of the other two.

La solution selon l'invention permet la réalisation d'un dépôt par cémentation en pack sur des pièces de géométrie complexe et dans des cavités difficilement accessibles.  The solution according to the invention allows the realization of a deposit by pack cementation on parts of complex geometry and in inaccessible cavities.

Le cément utilisé dans le cadre de l'invention présente une très bonne coulabilité permettant de remplir les plus petits interstices (de diamètre < 1mm) et se répartir de manière homogène à l'intérieur de l'ensemble de la cavité à revêtir. La distribution granulométrique et la morphologie des particules de cément sont les paramètres principaux pour assurer une bonne coulabilité du mélange.  The cementum used in the context of the invention has a very good flowability to fill the smallest gaps (diameter <1mm) and distribute evenly within the entire cavity to be coated. The particle size distribution and the morphology of the cement particles are the main parameters to ensure a good flowability of the mixture.

La distribution granulométrique est ajustée en fonction du diamètre équivalent du plus petit passage de la cavité. Concernant la morphologie, on favorise également les formes sphériques qui peuvent être obtenues par différentes techniques de broyage des poudres ou du mélange de poudre. Un traitement d' atomisation du mélange de poudre pourra également être utilisé pour former des sphères du mélange de poudre. Dans ce dernier cas, des additifs organiques pourront être utilisés pour assurer une bonne cohésion des sphères et une dispersion homogène des éléments du mélange. The particle size distribution is adjusted according to the equivalent diameter of the smallest passage of the cavity. With regard to morphology, spherical shapes which can be obtained by different grinding techniques for powders or powder mixture. An atomization treatment of the powder mixture may also be used to form spheres of the powder mixture. In the latter case, organic additives may be used to ensure a good cohesion of the spheres and a homogeneous dispersion of the elements of the mixture.

La présente invention a également pour objet deux procédés de dépôt d'un revêtement par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm. The present invention also relates to two methods of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm .

Le premier procédé de dépôt d'un revêtement par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm comprend les étapes successives suivantes : The first method of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm comprises the following successive steps:

a) on prépare un cément constitué de particules sphériques d'un agent activant, d'un diluant inerte et d'une poudre métallique, lesdites particules sphériques présentant chacune un diamètre d tel que d < ecm/10; a) preparing a cementum consisting of spherical particles of an activating agent, an inert diluent and a metal powder, said spherical particles each having a diameter d such that d <e cm / 10;

b) on introduit dans les cavités du substrat le cément préparé à l'étape a) par un système vibratoire ;  b) introducing into the cavities of the substrate the cementum prepared in step a) by a vibratory system;

c) on chauffe l'ensemble substrat - cément à une température inférieure à la température de fusion de la poudre métallique pendant une durée d'au moins 6h à environ 650°C pour l'aluminium.  c) the substrate-cement element is heated to a temperature below the melting temperature of the metal powder for a period of at least 6 hours at about 650 ° C for aluminum.

d) on refroidit l'ensemble substrat-cément à la température ambiante  d) the substrate-cement element is cooled to room temperature

e) on soumet le cément à une étape de vibration de manière à éliminer le résidu de cément,  e) the cementum is subjected to a vibration step so as to eliminate the cement residue,

f) on chauffe l'ensemble substrat-cément à une température compris entre 900°C et 1150°C, de préférence supérieure à 980°C, et  f) the substrate-cement element is heated to a temperature of between 900 ° C. and 1150 ° C., preferably greater than 980 ° C., and

g) on récupère un substrat présentant sur son ensemble un revêtement.  g) recovering a substrate having a coating as a whole.

A titre d'exemple si la poudre métallique est de l'aluminium, à l'étape c) on chauffe l'ensemble substrat-cément à environ 650°C pendant au moins 6h.  For example, if the metal powder is aluminum, in step c) the substrate-cement element is heated at about 650 ° C. for at least 6 hours.

Selon le cas, le premier procédé peut présenter une ou plusieurs des caractéristiques suivantes :  Depending on the case, the first method may have one or more of the following characteristics:

- les particules du cément préparé à l'étape a) sont pré-activées par mécano synthèse ; la préactivation permet d'augmenter la réactivité chimique des particules de précurseurs. the particles of the cementum prepared in step a) are pre-activated by mechano-synthesis; preactivation makes it possible to increase the chemical reactivity of the precursor particles.

Ce traitement facilite la réaction entre le précurseur et l'activateur et donc le dépôt. This treatment facilitates the reaction between the precursor and the activator and therefore the deposition.

- le revêtement récupéré à l'étape g) comprend du NiAl ;  the coating recovered in step g) comprises NiAl;

- le revêtement récupéré à l'étape g) présente une épaisseur comprise entre 15 et the coating recovered in step g) has a thickness of between 15 and

25 μιη. Le second procédé de dépôt d'un revêtement par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm comprend les étapes successives suivantes : 25 μιη. The second method of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm comprises the following successive steps:

a) on prépare un cément constitué d'un flux de décapage et de particules sphériques d'un diluant inerte et d'une poudre métallique, lesdites particules sphériques présentant chacune un diamètre d tel que d < ecm/10 ; a) a cementitious consisting of a stripping flux and spherical particles of an inert diluent and a metal powder is prepared, said spherical particles each having a diameter d such that d <e cm / 10;

b) on introduit dans les cavités du substrat le cément préparé à l'étape a) par un système vibratoire ;  b) introducing into the cavities of the substrate the cementum prepared in step a) by a vibratory system;

c) on chauffe l'ensemble substrat - cément à une température supérieure à la température de fusion du flux de décapage, sous vide primaire ou sous atmosphère inerte (Ar), pendant une durée comprises entre 10 min et 2h ;  c) the substrate-cementation unit is heated to a temperature above the melting temperature of the pickling stream, under a primary vacuum or under an inert atmosphere (Ar), for a period of between 10 min and 2 h;

d) on refroidit l'ensemble substrat-cément jusqu'à température ambiante  d) the substrate-cement element is cooled to room temperature

e) on soumet le cément à une étape de lavage de manière à éliminer le résidu de cément ;  e) the cement is subjected to a washing step so as to remove the cement residue;

f) on récupère un substrat présentant sur son ensemble un revêtement.  f) recovering a substrate having on its assembly a coating.

Selon le cas, le second procédé peut présenter une ou plusieurs des caractéristiques suivantes :  As the case may be, the second method may have one or more of the following characteristics:

- l'étape e) de lavage est réalisée au moyen d'une solution aqueuse acidifiée.  the washing step e) is carried out by means of an acidified aqueous solution.

- le revêtement récupéré à l'étape f) comprend du NiAl3. the coating recovered in step f) comprises NiAl 3 .

- ledit procédé comprend avant l'étape e) une étape de chauffage de l'ensemble substrat-cément à une température comprise entre 900°C et 1150°C, de préférence supérieure à 980°C  said process comprises, before step e), a step of heating the substrate-cementation unit at a temperature of between 900 ° C. and 1150 ° C., preferably greater than 980 ° C.

- le revêtement récupéré à l'étape f) comprend du NiAl.  the coating recovered in step f) comprises NiAl.

- le revêtement récupéré à l'étape f) présente une épaisseur comprise entre 5 μιη et 200μιη, de préférence entre 5 μιη et 80 μιη.  - The coating recovered in step f) has a thickness between 5 μιη and 200μιη, preferably between 5 μιη and 80 μιη.

La figure 1 schématise les différentes étapes du premier procédé selon l'invention. Figure 1 shows schematically the different steps of the first method according to the invention.

Le premier procédé consiste en l'utilisation d'un mélange pulvérulent constitué de l'agent activant (5%), d'un diluant inerte (Alumine, silice, ...) et d'un métal à déposer, une poudre métallique (entre 10 et 60%) qui peut être soit de l'aluminium pur ou un mélange Al +NÏA1 ou AlCr et dont les particules peuvent avoir ou non été "pré-activées" par mécano-synthèse. The first process consists in the use of a powder mixture consisting of the activating agent (5%), an inert diluent (Alumina, silica, etc.) and a metal to be deposited, a metal powder ( between 10 and 60%) which may be either pure aluminum or an Al + NIA1 or AlCr mixture and whose particles may or may not have been "pre-activated" by mechano-synthesis.

La granulométrie du mélange est alors ajustée de façon à ce qu'il puisse être introduit dans les canaux par un système vibratoire. L'ensemble est alors porté à une température inférieure à la température de fusion du métal à déposer pendant une durée d'au moins 6h00. Après refroidissement, l'ensemble est de nouveau soumis à une étape de vibration permettant l'extraction de la poudre résiduelle. A ce stade, le revêtement consiste en un enrichissement superficiel en aluminium du substrat dont la composition est proche de NiAl3. Les épaisseurs obtenues varient entre 5 et 10 μιη selon la durée durant laquelle on a réalisé la première étape de chauffage. Après cette étape, la pièce ainsi revêtue est portée à une température comprise entre 900°C et 1150°C, de préférence supérieure à 980°C de façon à obtenir la composition NiAl dans un liséré superficiel d'épaisseur allant de 15 à 25μιη (figure 3). The granulometry of the mixture is then adjusted so that it can be introduced into the channels by a vibratory system. The assembly is then brought to a temperature below the melting temperature of the metal to be deposited for a period of at least 6 hours. After cooling, the assembly is again subjected to a vibration step for extracting the residual powder. At this stage, the coating consists of a surface enrichment of aluminum substrate whose composition is close to NiAl 3 . The thicknesses obtained vary between 5 and 10 μιη depending on the time during which the first heating step was carried out. After this step, the part thus coated is brought to a temperature of between 900 ° C. and 1150 ° C., preferably greater than 980 ° C., so as to obtain the NiAl composition in a superficial edge of thickness ranging from 15 to 25 μm ( Figure 3).

La figure 2 schématise des différentes étapes du second procédé selon l'invention. Le second procédé consiste en l'utilisation d'un mélange pulvérulent constitué d'un flux de décapage à bas point de fusion (K A1F6-KA1F4) c'est l'élément qui a le point de fusion le plus faible du mélange constituant le cément et de particules d'un diluant inerte et d'une poudre métallique pur ou d'alliage d'aluminium. (10 à 60% de poudres métalliques, 40% de flux de décapage et le complément en diluant inerte). FIG. 2 schematizes the different steps of the second method according to the invention. The second method consists in the use of a powder mixture consisting of a low-melting pickling flux (K A1F 6 -KA1F 4 ) which is the element which has the lowest melting point of the mixture constituting the cement and particles of an inert diluent and a pure metal powder or aluminum alloy. (10 to 60% of metal powders, 40% of stripping flux and the balance of inert diluent).

Le tout est introduit par vibration comme dans le cas du premier procédé et est porté à haute température, inférieure à la fusion de la phase métallique, mais supérieure à celle du flux de décapage pendant un temps qui varie de quelques minutes à une ou deux heures.  The whole is introduced by vibration as in the case of the first method and is heated to a high temperature, lower than the melting of the metal phase, but greater than that of the stripping flux for a time that varies from a few minutes to one or two hours. .

Notons que le revêtement est obtenu, soit sous vide primaire ou soit sous atmosphère contrôlée inerte (argon).  Note that the coating is obtained either under primary vacuum or inert controlled atmosphere (argon).

Les résidus sont alors extraits par lavage directement après l'étape de traitement thermique. Pour améliorer encore l'extraction des résidus, l'appareil peut être lavé avec une solution chimique (aqueuse acidifiée). Le revêtement ainsi obtenu correspond à une phase de composition proche de NiAl qui peut se transformer en NiAl lors d'une étape ultérieure de recuit à une température comprise entre 900°C et 1150°C, de préférence à 980°C. L'aspect du revêtement est montré par la figure 4.  The residues are then extracted by washing directly after the heat treatment step. To further improve the extraction of residues, the apparatus can be washed with a chemical solution (acidified aqueous). The coating thus obtained corresponds to a phase of composition close to NiAl which can be converted into NiAl in a subsequent annealing step at a temperature between 900 ° C and 1150 ° C, preferably at 980 ° C. The appearance of the coating is shown in FIG.

Les mélanges de poudres peuvent être stockés sur de longues durées en dessiccateur sous vide primaire voire en enceinte sèche sous balayage de gaz neutre et sont aussitôt prêts à l'emploi.  The powder mixtures can be stored for long periods of time in a desiccator under a primary vacuum or in a dry chamber under a neutral gas sweep and are immediately ready for use.

De préférence, le diluant inerte est choisi parmi les poudres de matériaux inertes réfractaires, de préférence encore parmi les oxydes minéraux réfractaires, tels que l'alumine, la silice, la magnésie et leurs mélanges, qui sont couramment utilisés dans les traitements de pack-cémentation.  Preferably, the inert diluent is selected from powders of refractory inert materials, more preferably from refractory mineral oxides, such as alumina, silica, magnesia and mixtures thereof, which are commonly used in cementation.

Le substrat qui peut être pourvu d'un tel revêtement est généralement choisi parmi les substrats métalliques, par exemple base fer ou nickel, les substrats en alliage(s) ou en superalliage(s), les substrats composites comprenant un ou plusieurs métaux et/ou alliage(s) et/ou superalliage(s) contenant du Ni pour réagir avec l'Ai déposé et former le NiAl. The substrate which can be provided with such a coating is generally chosen from metal substrates, for example iron or nickel base, alloy (s) substrates or superalloy (s), composite substrates comprising one or more metals and / or alloy (s) and / or superalloy (s) containing Ni to react with the deposited Al and form NiAl.

En fonction de l'épaisseur de revêtement désiré, le substrat pourra être préalablement enrichi superficiellement en Ni par exemple par un dépôt électrolytique.  Depending on the desired coating thickness, the substrate may be previously superficially enriched in Ni for example by electrolytic deposition.

A titre d'exemples de pièces sur lesquelles on peut mettre en œuvre les procédés de dépôt selon l'invention, ont peut citer l'intérieur de tubes, les aubes de turbines, des échangeurs de chaleur, en particulier les échangeurs de chaleur métalliques, des échangeurs réacteur, des capacités de stockages, ....  By way of examples of parts on which the deposition processes according to the invention can be implemented, mention may be made of the interior of tubes, turbine blades, heat exchangers, in particular metal heat exchangers, reactor exchangers, storage capacities, ....

Les traitements sont généralement réalisés sous atmosphère neutre ou réductrice par exemple sous atmosphère d'hydrogène et/ou d'argon, de préférence sous atmosphère d'argon, ou encore sous une atmosphère d'argon avec par exemple de 5 à 10% d'hydrogène.  The treatments are generally carried out under a neutral or reducing atmosphere, for example under an atmosphere of hydrogen and / or argon, preferably under an argon atmosphere, or under an argon atmosphere with, for example, from 5 to 10% of argon. hydrogen.

La pression mise en œuvre pendant le traitement peut être la pression atmosphérique ou une pression réduite par exemple une pression de 10" atm d'argon. The pressure used during the treatment may be atmospheric pressure or a reduced pressure, for example a pressure of 10 " atm of argon.

Les revêtements obtenus par les procédés selon l'invention confèrent aux substrats une excellente résistance à la corrosion et ceci même au sein de chaque cavité de substrat indépendamment de sa taille.  The coatings obtained by the processes according to the invention give the substrates an excellent resistance to corrosion, even within each substrate cavity regardless of its size.

En conséquence, la durée de vie de ces substrats est sensiblement améliorée.  As a result, the service life of these substrates is substantially improved.

EXEMPLE EXAMPLE

Les photos de la figure 3 montrent deux échantillons d'alliage HR120, l'un (celui de droite) revêtu avec le revêtement élaboré suivant le second procédé selon l'invention et l'autre (celui de gauche) non revêtu. Ces échantillons ont été soumis à une atmosphère corrosive constituée de (en %vol.) : 15%CO, 5%C02, 55%H2, 25%H20, à une pression de 21 bars absolus et une température de 650°C. Après 4700 heures d'exposition, il apparaît clairement que le revêtement déposé selon le second procédé de l'invention permet de protéger l'alliage de la corrosion. The photos of FIG. 3 show two samples of HR120 alloy, one (the one on the right) coated with the coating produced according to the second method according to the invention and the other (the left one) uncoated. These samples were subjected to a corrosive atmosphere consisting of (in% vol.): 15% CO, 5% CO 2 , 55% H 2 , 25% H 2 O, at a pressure of 21 bar absolute and a temperature of 650 ° C. After 4700 hours of exposure, it is clear that the coating deposited according to the second method of the invention can protect the alloy from corrosion.

Claims

Revendications claims 1. Utilisation d'un cément dans un procédé de dépôt par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm, caractérisé en ce que le cément est constitué de particules sphériques présentant chacune un diamètre d tel que d≤ecm/10. 1. Use of a cementum in a deposition process by pack cementation on a substrate having cavities of minimum equivalent diameter e cm , characterized in that the cement consists of spherical particles each having a diameter d such that d e e cm / 10. 2. Utilisation selon la revendication 1, caractérisée en ce que le cément est constitué de particules sphériques présentant chacune un diamètre d tel que d < ecm/ 10. 2. Use according to claim 1, characterized in that the cementum consists of spherical particles each having a diameter d such that d <e cm / 10. 3. Utilisation selon l'une des revendications 1 ou 2, caractérisé en ce que le cément comprend un précurseur de l'élément à déposer, un agent activant et un diluant inerte. 3. Use according to one of claims 1 or 2, characterized in that the cement comprises a precursor of the element to be deposited, an activating agent and an inert diluent. 4. Utilisation selon la revendication 3, caractérisée en ce que le cément comprend :4. Use according to claim 3, characterized in that the cement comprises: - 10 à 60% de poudre métallique comme précurseur de l'élément à déposer, 10 to 60% of metal powder as precursor of the element to be deposited, - 5 à 40% d'agent activant, et  5 to 40% of activating agent, and - un complément à 100% de diluant inerte.  a complement to 100% of inert diluent. 5. Utilisation selon la revendication 4, caractérisée en ce que la poudre métallique est constituée d'aluminium ou d'un mélange d'aluminium avec des particules de NixAly ou de Alx'Cry' . 5. Use according to claim 4, characterized in that the metal powder is made of aluminum or a mixture of aluminum with Ni x Al y particles or Alx'Cry '. 6. Utilisation selon l'une des revendications 1 ou 2, caractérisée en ce que le cément comprend un précurseur de l'élément à déposer, un flux de décapage, et un diluant inerte. 6. Use according to one of claims 1 or 2, characterized in that the cement comprises a precursor of the element to be deposited, a stripping flux, and an inert diluent. 7. Utilisation selon l'une des revendications 1 à 6, caractérisée en ce que le cément comprend un liant organique ou inorganique. 7. Use according to one of claims 1 to 6, characterized in that the cement comprises an organic or inorganic binder. 8. Utilisation selon l'une des revendications 1 à 7, caractérisée en ce que le substrat est un échangeur de chaleur métallique. 8. Use according to one of claims 1 to 7, characterized in that the substrate is a metal heat exchanger. 9. Procédé de dépôt d'un revêtement par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm, comprenant les étapes successives suivantes : 9. A method of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm , comprising the following successive steps: a) on prépare un cément constitué de particules sphériques d'un agent activant, d'un diluant inerte et d'une poudre métallique, lesdites particules sphériques présentant chacune un diamètre d tel que d < ecm/10; a) preparing a cementum consisting of spherical particles of an activating agent, an inert diluent and a metal powder, said spherical particles each having a diameter d such that d <e cm / 10; b) on introduit dans les cavités du substrat le cément préparé à l'étape a) par un système vibratoire ;  b) introducing into the cavities of the substrate the cementum prepared in step a) by a vibratory system; c) on chauffe l'ensemble substrat - cément à une température inférieure à la température de fusion de la poudre métallique pendant une durée d'au moins 6h à environ c) the substrate-cement material is heated to a temperature below the melting temperature of the metal powder for a period of at least 6 hours to approximately 650°C pour l'aluminium. 650 ° C for aluminum. d) on refroidit l'ensemble substrat-cément à la température ambiante  d) the substrate-cement element is cooled to room temperature e) on soumet le cément à une étape de vibration de manière à éliminer le résidu de cément,  e) the cementum is subjected to a vibration step so as to eliminate the cement residue, f) on chauffe l'ensemble substrat-cément à une température compris entre 900°C et f) the substrate-cement element is heated to a temperature of between 900 ° C. and 1150°C, de préférence supérieure à 980°C, et 1150 ° C, preferably greater than 980 ° C, and g) on récupère un substrat présentant sur son ensemble un revêtement.  g) recovering a substrate having a coating as a whole. 10. Procédé de dépôt selon la revendication 9, caractérisé en ce que les particules du cément préparé à l'étape a) sont pré-activées par mécano synthèse. 10. Deposition process according to claim 9, characterized in that the particles of the cementum prepared in step a) are pre-activated by mechano-synthesis. 11. Procédé de dépôt selon l'une des revendications 9 ou 10, caractérisé en ce que le revêtement récupéré à l'étape g) comprend du NiAl. 11. The deposition method according to one of claims 9 or 10, characterized in that the coating recovered in step g) comprises NiAl. 12. Procédé de dépôt selon l'une des revendications 9 à 11, caractérisé en ce que le revêtement récupéré à l'étape g) présente une épaisseur comprise entre 15 et 25 μιη. 12. deposition process according to one of claims 9 to 11, characterized in that the coating recovered in step g) has a thickness between 15 and 25 μιη. 13. Procédé de dépôt d'un revêtement par pack-cémentation sur un substrat présentant des cavités de diamètre équivalent minimum ecm, comprenant les étapes successives suivantes : 13. A method of depositing a coating by pack cementation on a substrate having cavities of minimum equivalent diameter e cm , comprising the following successive steps: a) on prépare un cément constitué d'un flux de décapage et de particules sphériques d'un diluant inerte et d'une poudre métallique, lesdites particules sphériques présentant chacune un diamètre d tel que d < ecm/10 ; b) on introduit dans les cavités du substrat le cément préparé à l'étape a) par un système vibratoire ; a) a cementitious consisting of a stripping flux and spherical particles of an inert diluent and a metal powder is prepared, said spherical particles each having a diameter d such that d <e cm / 10; b) introducing into the cavities of the substrate the cementum prepared in step a) by a vibratory system; c) on chauffe l'ensemble substrat - cément à une température supérieure à la température de fusion du flux de décapage, sous vide primaire ou sous atmosphère inerte (Ar), pendant une durée comprises entre 10 min et 2h ;  c) the substrate-cementation unit is heated to a temperature above the melting temperature of the pickling stream, under a primary vacuum or under an inert atmosphere (Ar), for a period of between 10 min and 2 h; d) on refroidit l'ensemble substrat-cément jusqu'à température ambiante  d) the substrate-cement element is cooled to room temperature e) on soumet le cément à une étape de lavage de manière à éliminer le résidu de cément ;  e) the cement is subjected to a washing step so as to remove the cement residue; f) on récupère un substrat présentant sur son ensemble un revêtement.  f) recovering a substrate having on its assembly a coating. 14. Procédé selon la revendication 13, caractérisé en ce que l'étape e) de lavage est réalisée au moyen d'une solution aqueuse acidifiée. 14. The method of claim 13, characterized in that the washing step e) is carried out by means of an acidified aqueous solution. 15. Procédé selon l'une des revendications 13 ou 14, caractérisé en ce que le revêtement récupéré à l'étape f) comprend du NiAl3. 15. Method according to one of claims 13 or 14, characterized in that the coating recovered in step f) comprises NiAl 3 . 16. Procédé selon l'une des revendications 13 ou 14, caractérisé en ce que ledit procédé comprend avant l'étape e) une étape de chauffage de l'ensemble substrat-cément à une température comprise entre 900°C et 1150°C, de préférence supérieure à 980°C. 16. Method according to one of claims 13 or 14, characterized in that said method comprises before step e) a step of heating the substrate-cement unit at a temperature between 900 ° C and 1150 ° C, preferably greater than 980 ° C. 17. Procédé selon la revendication 16, caractérisé en ce que le revêtement récupéré à l'étape f) comprend du NiAl. 17. The method of claim 16, characterized in that the coating recovered in step f) comprises NiAl. 18. Procédé selon l'une des revendications 13 à 17, caractérisé en ce que le revêtement récupéré à l'étape f) présente une épaisseur comprise entre 5 μιη et 200μιη, préférentiellement entre 5 μιη et 80μιη. 18. Method according to one of claims 13 to 17, characterized in that the coating recovered in step f) has a thickness between 5 μιη and 200μιη, preferably between 5 μιη and 80μιη. 19. Procédé selon l'une des revendications 9 à 18, caractérisé en ce que le substrat est un échangeur de chaleur métallique. 19. Method according to one of claims 9 to 18, characterized in that the substrate is a metal heat exchanger.
EP14708611.0A 2013-02-13 2014-02-04 Method for depositing a corrosion-protection coating Active EP2956566B1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1351227A FR3001976B1 (en) 2013-02-13 2013-02-13 METHOD FOR DEPOSITING COATING AGAINST CORROSION
PCT/FR2014/050193 WO2014125187A1 (en) 2013-02-13 2014-02-04 Method for depositing a corrosion-protection coating

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EP2956566A1 true EP2956566A1 (en) 2015-12-23
EP2956566B1 EP2956566B1 (en) 2016-11-23

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EP (1) EP2956566B1 (en)
JP (1) JP2016510089A (en)
CN (1) CN105164303B (en)
FR (1) FR3001976B1 (en)
WO (1) WO2014125187A1 (en)
ZA (1) ZA201505484B (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023180085A1 (en) 2022-03-23 2023-09-28 Fives Cryo Method for coating the inner surfaces of a heat exchanger with a powdery solid catalyst

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3062324B1 (en) * 2017-01-30 2019-03-22 Safran Aircraft Engines PROCESS FOR MANUFACTURING PARTS PRODUCED IN METALLURGY OF POWDERS COMPRISING THE APPLICATION OF A COATING
KR102694701B1 (en) * 2022-11-09 2024-08-13 한국생산기술연구원 Method for coating object using pack cementation slurry composition and pack cementation slurry composition for base material coating therefor
KR102694721B1 (en) * 2022-11-09 2024-08-13 한국생산기술연구원 Method for coating mold using slurry pack cementation process and pack cementation slurry composition for mold coating therefor

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1379731A (en) * 1971-01-05 1975-01-08 Albright & Wilson Chromising ferrous metal substrates
DE2438405A1 (en) * 1973-08-13 1975-02-27 Albright & Wilson NON-ALLOY, LOW CARBON, STAINLESS STEELS AND THEIR INCHROMED PRODUCTS
US4156042A (en) * 1975-04-04 1979-05-22 The Secretary Of State For Defence In Her Britannic Majesty's Government Of The United Kingdom Of Great Britain And Northern Ireland Coating articles having fine bores or narrow cavities in a pack-cementation process
JPS62212100A (en) * 1986-03-14 1987-09-18 Canon Inc Powder filling method and equipment used in the method
DE4035790C1 (en) * 1990-11-10 1991-05-08 Mtu Muenchen Gmbh
EP0496935B1 (en) * 1991-01-31 1995-04-19 General Electric Company Aluminide processing of articles protected by a thermal barrier coating system
US5441767A (en) * 1994-01-26 1995-08-15 United Technologies Corporation Pack coating process for articles containing small passageways
JPH10298779A (en) * 1997-04-25 1998-11-10 Hitachi Ltd Gas turbine bucket manufacturing method
DE19856901C2 (en) * 1998-12-10 2003-01-16 Mtu Aero Engines Gmbh Process for coating hollow bodies
US6299935B1 (en) * 1999-10-04 2001-10-09 General Electric Company Method for forming a coating by use of an activated foam technique
JP2001254163A (en) * 2000-12-18 2001-09-18 Ichiro Kawakatsu METHOD OF COATING Ni OR Ni ALLOY SUBSTRATE WITH Al OR Al ALLOY
US7094445B2 (en) * 2002-05-07 2006-08-22 General Electric Company Dimensionally controlled pack aluminiding of internal surfaces of a hollow article
GB0409486D0 (en) * 2004-04-28 2004-06-02 Diffusion Alloys Ltd Coatings for turbine blades
US7252480B2 (en) * 2004-12-17 2007-08-07 General Electric Company Methods for generation of dual thickness internal pack coatings and objects produced thereby
JP5403881B2 (en) * 2007-07-10 2014-01-29 ゼネラル・エレクトリック・カンパニイ Aluminizing method of serpentine cooling passage of jet engine blade
FR2921937B1 (en) * 2007-10-03 2009-12-04 Snecma METHOD FOR STEAM PHASE ALUMINIZATION OF A TURBOMACHINE METAL PIECE
US8501273B2 (en) * 2008-10-02 2013-08-06 Rolls-Royce Corporation Mixture and technique for coating an internal surface of an article
JP2010112671A (en) * 2008-11-10 2010-05-20 Showa Denko Kk Method of manufacturing tube for heat exchanger

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2014125187A1 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2023180085A1 (en) 2022-03-23 2023-09-28 Fives Cryo Method for coating the inner surfaces of a heat exchanger with a powdery solid catalyst
FR3133769A1 (en) 2022-03-23 2023-09-29 Fives Cryo METHOD FOR COATING INTERNAL SURFACES OF AN EXCHANGER WITH A POWDERED SOLID

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CN105164303B (en) 2018-04-20
EP2956566B1 (en) 2016-11-23
FR3001976B1 (en) 2015-02-20
US20150368782A1 (en) 2015-12-24
CN105164303A (en) 2015-12-16
JP2016510089A (en) 2016-04-04
WO2014125187A1 (en) 2014-08-21
ZA201505484B (en) 2016-04-28
FR3001976A1 (en) 2014-08-15

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